Federal Register of Legislation - Australian Government

Primary content

AD/BELL 222/37 - Tail Rotor Pitch Change Mechanism

Authoritative Version
AD/BELL/222/37 Airworthiness Directives/Pt 105 — Aircraft as made
Tail Rotor Pitch Change Mechanism
Administered by: Infrastructure, Transport, Regional Development and Communications
Exempt from sunsetting by the Legislation (Exemptions and Other Matters) Regulation 2015 s12 item 15
Registered 06 Jul 2007
Tabling HistoryDate
Tabled HR07-Aug-2007
Tabled Senate07-Aug-2007
Enabled by
Authoritative version Civil Aviation Safety Regulations 1998
F1998B00220SR 1998 No. 237